An interpretation of L' combustion instability in terms of acoustic instability theory.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (6) , 1097-1102
- https://doi.org/10.2514/3.4143
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Experimental solid rocket combustion instabilitySymposium (International) on Combustion, 1965
- Theory of acoustic instability in solid-propellant rocket combustionSymposium (International) on Combustion, 1965
- T-burner method of determining the acoustic admittance of burning propellantsAIAA Journal, 1964
- A theory of low-frequency combustion instability in solid rocket motorsAIAA Journal, 1964
- LOW PRESSURE ROCKET EXTINCTIONAIAA Journal, 1963
- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961